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On the structural dynamics of laminated composite plates and sandwich structures; a new perspective on damping identification

机译:叠层复合板与夹层结构的结构动力学; 一种关于阻尼识别的新视角

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This paper presents the modelling and the dynamic characterisation of laminated composite plates and sandwich structures in terms of stiffness and damping. The developments used in this paper are based on the analytical multilayer model of Guyader and Lesueur (JSV, 1978). The model considers linear shear, membrane and bending effects in each layer. The characteristics of the structure are determined by means of an equivalent thin plate methodology. The first main novelty of this paper consists in adapting this methodology for laminated plates (orthotropic multilayers with arbitrary orthotropic angle per layer). An experimental validation of this adaptation is presented for a laminated composite plate. Concerning the modelling of the structural loss factor, a space domain definition based on the spatial attenuation of a plane wave is compared to an energetic method and an equivalent definition based on the thin plate theory. The results show that the equivalent definition overestimates the loss factor in high frequencies since the thin plate theory only considers the flexural behaviour of the structure. On the contrary, the space domain definition (which give similar results as compared to the energetic one for lightly damped structures) considers the frequency dependent variation of the dynamic behaviour of the structure by means of the ratio between the group and phase velocities. The latter approach is considered to be more correct. The second main novelty of this article is on the experimental validation of this space domain definition. The structural loss factors of two sandwich structures are identified from measurements using modal, energetic and spatial methods. The results using the space domain definition are in very good agreement with the analytical predictions and the estimations of the modal and energetic methods for both plates for a large frequency band (up to 20 kHz), demonstrating the validity of the approach developed in this paper. (C) 2020 Elsevier Ltd. All rights reserved.
机译:本文介绍了层压复合板和夹层结构的建模和动态表征,刚度和阻尼方面。本文使用的发展基于Guyader和Lesueur的分析多层模型(JSV,1978)。该模型考虑每层的线性剪切,膜和弯曲效应。结构的特性通过等同的薄板方法确定。本文的第一个主要新颖性包括适应该方法的层压板(每层具有任意正交角度的正交多层)。提出了这种适应的实验验证,用于层压复合板。关于结构损失因子的建模,基于平面波的空间衰减的空间域定义与基于薄板理论的能量方法和等同的定义进行了比较。结果表明,由于薄板理论仅考虑结构的弯曲行为,所以等效的定义高估了高频处的损耗因子。相反,空间域定义(与用于轻微阻尼结构的能量之一相比提供类似的结果)通过基团和相速度之间的比率来借助于该结构的动态行为的频率相关变化。后一种方法被认为是更正确的。本文的第二个主要新颖性是对此空间域定义的实验验证。使用模态,能量和空间方法测量的两个夹层结构的结构损失因子。使用空间域定义的结果与用于大频带(高达20 kHz)的平板(高达20 kHz)的模板预测和模态和能量方法的估计非常好,展示了本文开发的方法的有效性。 (c)2020 elestvier有限公司保留所有权利。

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